<DOC>
<DOCNO>
306
</DOCNO>
<TITLE>
second approximation to laminar compressible boundary
layer on flat plate in slip flow .
</TITLE>
<AUTHOR>
maslen,s.h.
</AUTHOR>
<BIBLIO>
naca tn.2818, 1952.
</BIBLIO>
<TEXT>
  the first-order solution for the laminar compressible boundary-layer
flow over a flat plate at constant wall temperature is given .  the
effect of slip at the wall as well as the interaction between the
boundary-layer flow and the outer stream flow are taken into consideration
.  the solution is obtained explicitly in terms of the known zero
order, or continuum, solution .  no
assumptions regarding the prandtl number
or viscosity-temperature law need be made .  it is found that the
first-order solution gives a decrease in heat transfer and, for supersonic
flow, an increase in skin friction .
for subsonic flow there is no
first-order shear effect .  the change in heat transfer is due to slip
and the change in friction is due to the interaction of the zero- and
first-order velocities at the outer edge of the boundary layer .
</TEXT>
</DOC>
